//Version 6_2
[fltsim.0]
title=de Havilland DH104 Dove
sim=DH104_BW6_2
model=2
panel=
sound=
texture=OY-DHZ
kb_checklists=DH104_check
kb_reference=DH104_ref_2
ui_manufacturer=de Havilland
ui_type=DH-104 Dove
ui_variation=Cimber Air Dove
atc_heavy=0
atc_id=OY-DHZ
atc_airline=Cimber Air
atc_flight_number=348
description=Cimber Air Dove. The Dove was designed as a light transportation and training aircraft. More than 530 have been build from 1946 to 1964. OY-DHZ is a Dove 6, with two 400 hp Gipsy Queen motorer, its build on Hatfield, UK in 1956. It came to Denmark in 1969, were it was flying 10 years before it was deleted from register. It was owned by Cimber Air, Sønderborg, were it was flying passengers. When Cimber could´nt use it anymore, they gave it to Denmarks Flying Museeum. Repainted by Claus Vendelboe Holmberg May 2006.
[General]
atc_type=DeHavilland
atc_model=Dove
performance=Cruise Speed\n160 kts 296 km/hr\n\nEngine\nde Havilland Gypsy Queen 70-2 380 hp\n\nPropeller\nThree-bladed de Havilland constant-speed, variable pitch\n\nMaximum Range\n1000 mls \n\nService Ceiling\n20,000 ft \n\nFuel Capacity\n202 US gal\n\nMaximum Gross Weight\n8,800 lb 3,995 kg\n\nLength\n29 ft, 10 in 9.09 m\n\nWingspan\n37 ft, 10 in 11.53 m\n\nHeight\n9 ft, 9 in 2.97 m\n\nSeating Up to 10\n\nUseful Load\n1,860 lb 844 kg
prop_anim_ratio=.50
[WEIGHT_AND_BALANCE]
max_gross_weight = 8800.000
empty_weight = 5725.000
reference_datum_position = 0.0, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -1.5, 0.0, 0.0
max_number_of_stations = 11
station_load.0 = 170, 4.18, -1.04, 1.06, Pilot
station_load.1 = 170, 4.18, 1.04, 1.06, Co-pilot
station_load.2 = 170, 1.2, -1.2, 1.06, Passenger
station_load.3 = 170, 1.2, 1.2, 1.06, Passenger
station_load.4 = 170, -1.3, -1.2, 1.06, Passenger
station_load.5 = 170, -1.3, 1.2, 1.06, Passenger
station_load.6 = 170, -3.5, -1.2, 1.06, Passenger
station_load.7 = 170, -3.5, 1.2, 1.06, Passenger
station_load.8 = 0, -5.8, -1.2, 1.06, Passenger
station_load.9 = 0, -5.8, -1.2, 1.06, Passenger
station_load.10 = 140, -8, 0, 0, Baggage
;Moments of Inertia
empty_weight_pitch_MOI = 7958
empty_weight_roll_MOI = 9131
empty_weight_yaw_MOI = 15900
empty_weight_coupled_MOI = 0
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 0
Engine.0 = 6.800, -6.470, 0.000
Engine.1 = 6.800, 6.470, 0.000
fuel_flow_scalar= 1.1
min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine] //Based on Gypsy Queen 70-2
power_scalar =1.000
cylinder_displacement= 103.67
compression_ratio= 6.500
number_of_cylinders= 6
max_rated_rpm= 2980.000
max_rated_hp= 380.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.295
turbocharged= 1
max_design_mp= 45.000
min_design_mp= 7.000
critical_altitude= 4400.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 1
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[propeller]
rotation= -1,-1
thrust_scalar =1.000
propeller_type= 0
propeller_diameter= 7.5
propeller_blades= 3
propeller_moi=6.1
beta_max= 65.0
beta_min= 18.6
min_gov_rpm= 600
prop_tc= 0.006
gear_reduction_ratio= 1.4
fixed_pitch_beta= 25.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 88.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 1.000
minimum_reverse_beta= 0.000
[contact_points]
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1.000, 11.2129, 0.000, -5.15, 1600.000, 0.000, 0.8, 60.000, 0.08, 2.500, 0.850, 3.000, 3.000, 0.0, 152.000, 180.000
point.1 = 1.000, -2.1117, -6.789, -4.98, 1600.000, 1.000, 1.080, 0.000, 0.20, 2.500, 0.850, 4.100, 4.300, 2.0, 152.000, 200.000
point.2 = 1.000, -2.1117, 6.789, -4.98, 1600.000, 2.000, 1.080, 0.000, 0.20, 2.500, 0.850, 4.300, 4.100, 3.0, 152.000, 200.000
//SCRAPES
point.3 = 2, -26.443, -0.009, 1.362, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.4 = 2, 12.718, 0.000, -1.421, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.5 = 2, -1.370, -28.053, 0.769, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.6 = 2, -1.370, 28.053, 0.769, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
static_pitch = 0.99 //degrees (pitch when loaded on ground)
static_cg_height=5.01 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic//Pneumatic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 10.0 //Flap angle that activates warning at idle
flap_limit_power = 31.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.45 //Brake scalar
differential_braking_scale = 0.8 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 475.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[electrical]
max_battery_voltage = 24.0
engine_generator_map=1,1
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
electric_always_available = 0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 10, 17.0
pitot_heat = 0, 5 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
light_cabin = 0, 5 , 17.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 0, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[Views]
eyepoint = 4.3, -0.86, 3.35 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 1, -0.69, 0.00, -2.4, fx_beacon,
light.2 = 1, -9.35, 0.00, 3.8, fx_beacon,
light.3 = 4, 4.3, 0.0, 2.5, fx_vclight,
light.4 = 4, 0.0, 0.0, 3.0, fx_vclight,
light.5 = 4, -4.0, 0.0, 3.0, fx_vclight,
light.6 = 4, -9.0, 0.0, 2.8, fx_vclight,
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn and Bank
[fuel]
LeftMain = -0.4,-4,-1,101.05,2.4
RightMain = -0.4, 4,-1,101.05,2.4
fuel_type = 1
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup=fx_engstrt_dv
[airplane_geometry]
wing_area = 335.000
wing_span = 57.000
wing_root_chord = 8.660
wing_dihedral = 6.000
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor= 0.8776
wing_winglets_flag = 0
wing_sweep = 0.0
wing_pos_apex_lon = 2.165
wing_pos_apex_vert = 1.41
htail_area = 37.6
htail_span = 17.66
htail_pos_lon = -20.480
htail_pos_vert = 1.760
htail_incidence = 0.000
htail_sweep = 0
vtail_area = 19.03
vtail_span = 8.600
vtail_sweep = 0
vtail_pos_lon = -22.0
vtail_pos_vert = 3.450
elevator_area = 25.190
aileron_area = 22.46
rudder_area = 16.990
elevator_up_limit = 27.000
elevator_down_limit = 14.000
aileron_up_limit = 21.200
aileron_down_limit = 18.800
rudder_limit = 25.000
elevator_trim_limit = 20.000
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 65.0
full_flaps_stall_speed = 55.0
cruise_speed = 160.0
max_indicated_speed = 206.0 //Red line (KIAS)
max_mach = 0.51
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 900.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[stall_warning]
type=2
[Flaps.0]
type= 1
span-outboard= 0.550
extending-time= 7.000
system_type= 1
damaging-speed= 152.000
blowout-speed= 182.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 60.000, 0.000
[folding_wings]
wing_fold_system_type = 4
fold_rates = 0.12, 0.11
[TailHook]
tailhook_length = 4
tailhook_position = -15, 0, -1
cable_force_adjust = 1
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
